GE CFM56 series
Service difficulty reports · 5,028
Newest first. General aviation reporting is voluntary.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE engine_model_key = 'CFM56' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE engine_model_key = 'CFM56' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR SWAA022651Engine · flamed outNR 2 ENGINE FLAMEOUT, DECLARED EMERGENCY, AIR TURNBACK, NR 2 ENGINE FLAMED OUT DURING CLIMB. REMOVED AND REPLACED MEC AND FUEL PUMP, PROBLEMS STILL EXIST. REMOVED AND REPLACED NR 2 ENGINE PER MM.SDR 2002UALA01696Door · out of adjustAIRCRAFT RETURNED TO FIELD DUE TO VIBRATION FELT IN THE CONTROL CABIN. FOUND RIGHT NOSE DOOR IN AIRSTREAM WHEN GEAR UP. ADJUSTED DOOR. TROUBLESHOT AND FOUND NO OBVIOUS DISCREPANCIES. INSPECTED AS REQUIRED.SDR 2002UALA01669Skin · damagedRIGHT HAND HORIZONTAL STABILIZER LEADING EDGE HAD EXCESS MATERIAL REMOVED, 24 INCHES FROM FUSELAGE. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER.SDR 2002UALA01675Light · inoperativeEMERGENCY LIGHT AFT OF AFT ENTRY DOOR INOPERATIVE. RELAMP. OPERATIONS CHECK NORMAL.SDR 2002UALA01676Crease Beam · crackedNOSE FLIGHT DECK FLOOR STATION 196 RIGHT HAND CREASE BEAM WEB CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM WEB.SDR 2002UALA01677Crease Beam · crackedNOSE STATION 196 LEFT HAND CREASE BEAM WEB CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM WEB.SDR 2002UALA01678Frame · crackedBODY STATION 887, STRINGER 9R CABIN BODY FRAME CRACKED. MAJOR REPAIR ACCOMPLISHED. DOUBLER MANUFACTURED AND INSTALLED.SDR 2002UALA01679Frame · crackedBODY STATION 827, STRINGER 9L CABIN BODY FRAME WEB IS CRACKED. MAJOR REPAIR ACCOMPLISHED. DOUBLER MANUFACTURED AND INSTALLED.SDR 2002UALA01681Beam · gougedLEFT HAND MLG BEAM OUTBOARD END GOUGED FROM SPAR REPAIR FASTENER. MAJOR REPAIR ACCOMPLISHED. BLEND REPAIR ACCOMPLISHED.SDR 2002UALA01667Frame · crackedBODY STATION 867, STRINGER 9L, CABIN BODY FRAME WEB IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLER MANUFACTURED AND INSTALLED.SDR 2002UALA01668Frame · crackedCABIN FUSELAGE FRAME WEB STA 867 IS CRACKED AT STRINGER 9R. MAJOR REPAIR ACCOMPLISHED. INSTALLED FRAME DOUBLER REPAIRSDR 2002UALA01647Frame · crackedCABIN BODY FRAME WEB IS CRACKED BODY STATION 827 STRINGER 9R. MAJOR REPAIR ACCOMPLISHED. SPLICED BODY FRAME WEB.SDR 2002UALA01648Intercostal · crackedCABIN BODY FRAME INTERCOSTAL ASSEMBLY IS CRACKED BODY STATION 291 JUST BELOW STRINGER 10R. MAJOR REPAIR ACCOMPLISHED. REPLACED INTERCOSTAL ASSY.SDR 2002UALA01657Frame · crackedBODY STATION 616, LT FUSELAGE FRAME INBOARD CHORD ANGLE HAS 2 INCH CRACK 6 INCHES BELOW CREASE BEAM WEB WL 201. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED AND INSTALLED REPAIR DOUBLER.SDR 2002UALA01658Frame · crackedBODY STATION 847, STRINGER 9L CABIN BODY FRAME IS CRACKED. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED & INSTALLED DOUBLER.SDR 2002UALA01659Frame · crackedBODY STATION 847, STRINGER 9R CABIN BODY FRAME WEB IS CRACKED. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED & INSTALLED REPAIR DOUBLER.SDR 2002UALA01660Pressure Panel · crackedCABIN PRESSURE WEB CRACKED, STA 675,LBL 30. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR.SDR 2002UALA01646Skin · damagedFUSELAGE SKIN HAS SEVERAL HOLES DAMAGED AT NR 2 AIRPHONE ANTENNA BASE. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR 2002UALA01656Indicator · failedAIRCRAFT LANDED UNDER AMBER ALERT WHEN THE FLIGHT CREW WAS UNABLE TO EXTEND THE FLAPS BEYOND 10 DEGREES. FLAP POSITION INDICATOR INOPERATIVE. REPLACED FLAP POSITION INDICATOR.SDR 2002UALA01644Skin · damagedRIGHT HAND HORIZONTAL STABILIZER LEADING EDGE HAS EXCESSIVE MATERIAL LOSS AT BLEND 67 INCHES OB OF IB END. MAJOR REPAIR ACCOMPLISHED. INSTALLED FLUSH DOUBLER & FILLER.SDR 2002UALA01641Intercostal · crackedINTERCOSTAL CRACKED BETWEEN BS188 AND BS196 FUSELAGE FRAMES AT STRINGER 17 RIGHT HAND. MAJOR REPAIR ACCOMPLISHED. REPLACED INTERCOSTAL.SDR 2002UALA01634Skin · damagedLT HORIZONTAL STABILIZER LEADING EDGE SKIN HAS EXCESSIVE MATERIAL LOSS 50 INCHES FROM INBOARD END. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR 2002UALA01640Inverter · failedEMERGENCY ELECTRICAL LIGHTING STRIP INOPERATIVE THE LAST FOUR ROWS OF COACH. INOPERATIVE INVERTER AND POOR LIGHT STRIP CONNECTION.SDR AWXA200201140Wedge · delaminatedMAJOR REPAIR DURING C-19 CHECK, NR 4 LEADING EDGE SLAT INBOARD WEDGE WAS FOUND TO BE DELAMINATED. MAINTENANCE REMOVED AND REPLACED THE NR 4 LEADING EDGE SLAT IAW BMM. OPERATIONAL CHECK ACCOMPLISHED IAW BMM.SDR 2002UALA01620Pressure Panel · damagedRIGHT WHEEL WELL CEILING ABOVE THE SPOILER MIXER HAS EXCESSIVE MATERIAL REMOVED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR 2002UALA01622Skin · dentedRT HORIZONTAL STABILIZER LEADING EDGE APPROXIMATELY MIDWAY HAS A SERIES OF DENTS. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND FILLER AND REINSTALLED LEADING EDGE.SDR 2002UALA01623Overheat Loop · shortedWING BODY OVERHEAT LIGHT ILLUMINATED EN ROUTE, AND RETURNED TO FIELD. PERFORMED INSPECTION OF THE LEFT WING BODY OVERHEAT DETECTION SYSTEM AND FOUND A SHORT TO GROUND ON PIN 9 OF CONNECTOR D742. ISOLATED THE FAULT TO A SHORTED AFT KEEL BEAM DETECTOR M273. RSDR SWAA022523Engine · leakingIN-FLT SHUTDOWN, DECLARED EMERGENCY, NR 2 ENGINE OIL PRESS WENT TO 0, OIL QUANTITY DROPPED TO 0, SHUTDOWN ENGINE. REMOVED AND REPLACED NR 2 ENGINE PER MM.SDR 2002UALA01621Light · inoperativeEMERGENCY EXIT LIGHTS BETWEEN ROWS 3 AND 10 AND 17 TO THE AFT CABIN INOPERATIVE. REPLACED POWER STRIPSDR 2002UALA01614Relay · failedAIRCRAFT RETURNED TO FIELD WHEN NUMBER 2 GENERATOR CIRCUIT BREAKER TRIPPED, UNABLE TO RESET. REPLACED TRANSFER RELAYS R3 AND R4.SDR 2002UALA01615Rib · crackedRIGHT HAND HORIZONTAL STABILIZER LEADING EDGE MOST INBD RIB FLANGE IS CRACKED AT LOWER END. MAJOR REPAIR ACCOMPLISHED. REPLACED RIB CHORD.SDR ASAA024165Light · inoperativeEMERGENCY FLOOR LIGHTS ARE INOPERATIVE NEAR AFT LAVATORY AREA. RECONNECTED TRACK LIGHTS. TRACK LIGHTS THEN OPERATED NORMALLY.SDR 2002UALA01606Rib · dentedLEFT HAND HORIZONTAL STABILIZER APPROXIMATELY MID POINT HAS SERIES OF DENTS ACROSS RIB. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER.SDR 2002UALA01604Skin · damagedFUSELAGE SKIN AT STATION 807 STRINGER 17R HAS BLENDED AREA WITH EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. SKIN REPAIR.SDR 2002UALA01605Frame · gougedAFT PIT FRAME STATION 787 RBL 20 UPPER SURFACE GOUGED FROM SUPPORT STRAP. MAJOR REPAIR ACCOMPLISHED. FRAME CAP HOLE STRAP REPAIR.SDR 2003UALA00792Stringer · crackedSTRINGER 8 RT CRACKED AT FIVE CONSECUTIVE STRINGER CLIP LOCATIONS. STA 500, 500A, 500B, 500C, 500D. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED STRINGER FROM STA 500 TO 520, SPLICED IN STRINGER SECTION AND REPLACED CLIPS.SDR ASAA024164Light · disconnectedEMERGENCY FLOOR LIGHTS ARE INOPERATIVE AT ROWS 17-19. RECONNECTED TRACK LIGHTS. TRACK LIGHTS THEN OPERATED NORMALLY.SDR 2002UALA01602Skin · crackedCRACK IN FUSELAGE SKIN DOUBLER AT FORWARD EDGE OF FORWARD PIT DOOR CUTOUT 13 INCHES ABOVE LOWER EDGE. MAJOR REPAIR ACCOMPLISHED. TRIPLER REPAIR.SDR 2002UALA01603Door Frame · corrodedAFT CARGO COMPARTMENT DOOR CUTOUT FRAME AT BODY STATION 794 S23R TO S24R AFT SIDE HAS EXCESSIVE MATERIAL REMOVED TO CLEAN CORROSION. MAJOR REPAIR ACCOMPLISHED. FABRICATED REPAIR DOUBLER.SDR DL738021204Engine · bird ingestionON SHORT FINAL BIRD HIT FWD PORTION OF A/C . PERFORMED BIRD STRIKE INSPECTION AND BORESCOPE OF NR 1 ENGINE - ALL OKSDR USAASB02189Relay · faultyIN PREPARATION FOR LANDING, CREW RECEIVED BOTH THE RED AND GREEN NOSE LANDING GEAR LIGHTS AFTER GEAR EXTENSION. AFTER RECYCLING GEAR SEVERAL TIMES, CREW RECEIVED NORMAL GEAR INDICATION. FLIGHT LANDED NORMALLY, WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED ASDR 2002UALA01596Intercostal · crackedCABIN FLOOR INTERCOSTAL UPPER FLANGE CRACKED AT BODY STATION 933 BL 0. MAJOR REPAIR ACCOMPLISHED. REPLACED UPPER FLANGE.SDR 2002UALA01599Transmitter · failedAIRCRAFT DIVERTED EN ROUTE WHEN ENGINE NR 2 OIL PRESSURE INDICATOR SHOWED 0 PSI. OIL PRESSURE LIGHT WAS NOT ILLUMINATED. THE PROBLEM WAS ISOLATED TO THE OIL PRESSURE TRANSMITTER. IT WAS REPLACED AND SENT TO THE SHOP FOR TESTING. THE TRANSMITTER FAILED SHOPSDR 2002UALA01598Light · inoperativeEMERGENCY ELECTRICAL LIGHTING INOPERATIVE IN THE AFT CABIN. DEFECTIVE LAMP ASSEMBLY. RELAMPED.SDR SWA2002F00000Spar · crackedCRACK WAS FOUND DURING D CHECK VISUAL INSPECTION IN THE BACK SHOP. DISCOVERED THE MAIN SPAR CRACKED IN THE LOWER CHORD/WEB RADIUS COMMON TO THE OUTBOARD AFT FLAP TRACK ATTACH POINT. THE CIRCUMSTANCES UNDER WHICH IT OCCURED IS UNKNOWN. COULD BE FATIGUE OR ANSDR 2002UALA01585Skin · damagedEXTERNAL FUSELAGE SKIN HAS EXCESSIVE MATERIAL LOSS AFTER BLEND. 30 PERCENT LOSS AT LOWER AFT CORNER OF AFT ENTRY DOOR CUTOUT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER.SDR 2002UALA01586Skin · damagedEXTERNAL FUSELAGE SKIN, INTERNAL DOUBLER & STRAP WERE REPAIRED. MAJOR REPAIR ACCOMPLISHED. DOUBLER & TRIPLER REPAIR.SDR 2002UALA01592Angle · corrodedAFT GALLEY DOOR FUSELAGE CUTOUT LOWER SILL ZEE ANGLE INNER CHORD CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW ZEE ANGLE.SDR 2002UALA01587Tee Fitting · corrodedAFT PIT DOOR OPENING FORWARD FRAME TEE FITTING FOR BOTTOM STOP PAD FITTING IS CORRODED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. REPLACED SUPPORT TEE FITTING.SDR USAASB02187Charger · failedMAINTENANCE FOUND THE EMERGENCY LIGHTS AT SEATS 18 DEF THROUGH 20 DEF INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND CHARGER ASSEMBLY ABOVE SEAT ROW 20 DEF. OPERATIONAL CHECK OF EMERGENCY LIGHTS GOOD.
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